DocumentCode
2023059
Title
Optimal control method of stretching process of solar wings on multibody spacecraft
Author
Ge Xin-Sheng ; Chen Li-Qun
Author_Institution
Shanghai Inst. of Appl. Math. & Mech., Shanghai Univ.
Volume
1
fYear
2002
fDate
2002
Firstpage
255
Abstract
The optimal attitude control problem of spacecraft during the stretching process of solar wings is discussed in this paper. A mathematical model of the system is established by using the multibody dynamics and optical control theory. An algorithm of control for the stretching process is proposed, considering the nonholonomic behavior of the system. The effectiveness of the approach is shown by numerical simulation.
Keywords
attitude control; dynamics; nonlinear systems; optimal control; space vehicles; attitude control; mathematical model; multibody dynamics; nonholonomic system; optimal control; solar wings stretching; spacecraft; Attitude control; Control systems; Mathematical model; Mathematics; Numerical simulation; Optical control; Optimal control; Space vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Automation, 2002. Proceedings of the 4th World Congress on
Print_ISBN
0-7803-7268-9
Type
conf
DOI
10.1109/WCICA.2002.1022109
Filename
1022109
Link To Document